- Registered owner
- Courtney Aviaton LLC
- Location
- Columbia, CA
- Owner type
- LLC
- Serial number
- 11303
- Year built
- 1975
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 21, 1975
- Certificate issued
- April 2, 2026
- Expires
- April 30, 2033
- Mode S code
- AB9DC8
Rockwell International 690ATCDS 2A4Airframe · Rockwell International 690AEngine modelAiResearch TPE331-5&6SER
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 4 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 1 |
| 1984 | 1 |
| 1988 | 1 |
| 1994 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2010 | 1 |
| 2013 | 1 |
Airframe · Rockwell International 690A
AD 2013-09-05FuselageAD 2009-25-02Upper wing skinsAD 2006-15-01Inboard and center aileron hinge fittingsInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Rockwell International 690A
SAIB 2023-14Landing Gear Retract/Extend SystemNTSB investigations
No NTSB investigations matched to N848CEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Rockwell International 690A aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MV5RO55NBellcrank · failedTHE BELLCRANK FOR THE LT NOSE GEAR AFT DOOR FAILED/ CRACKED AT THE ROD END UPPER ATTACH POINT AND FELL OVER IN THE WHEEL WELL WHILE THE GEAR WAS IN THE UP POSITION. WHEN THE DOWN POSITION WAS SELECTED THE GEAR COULD NOT EXTEND DUE TO THE ROD BEING IN THE WAY.SDR 99ZZZX13Autopilot · misinstalledAUTOPILOT WOULD NOT CAPTURE NAV OR SLOW TO CAPTURE. AUTOPILOT WOULD DRIFT FROM PROPER COURSE WHEN CAPTURED. THIS WAS DUE TO INCORRECT HSI MODE RELAY INTERFACE WIRING FOR GPS. WIRING WAS INTERRUPTED AT AUTOPILOT FLIGHT DETECTOR INDICATOR FD 112V AND SHOULD H
STCs that may be installed · 169
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Rockwell International 690A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller